Accurate Navier-Stokes results for the hypersonic flow over a spherical nosetip
- 1 March 1990
- journal article
- research article
- Published by American Institute of Aeronautics and Astronautics (AIAA) in Journal of Spacecraft and Rockets
- Vol. 27 (2) , 113-122
- https://doi.org/10.2514/3.26115
Abstract
No abstract availableKeywords
This publication has 4 references indexed in Scilit:
- Introduction to computational techniques for boundary layersPublished by Office of Scientific and Technical Information (OSTI) ,1979
- On the solution of the unsteady Navier- Stokes equations including multicomponent finite rate chemistryComputers & Fluids, 1973
- Transitional and Turbulent Heat-Transfer Measurements on a Yawed Blunt Conical NosetipAIAA Journal, 1972
- VIII. The deferred approach to the limitPhilosophical Transactions of the Royal Society A, 1927